纤维缠绕复合材料约束球形浮力芯材准静态压缩吸能机制

针对海洋工程平台的防护吸能和浮力储备需求,设计一种纤维缠绕复合材料约束球形浮力芯材吸能结构。为分析其变形损伤特征和能量耗散机理,通过ABAQUS有限元软件和万能材料试验机开展数值模拟分析和试验验证研究。通过力学响应特征和损伤破坏模式分析可知,结构吸能设计的关键在于表层和芯材的泊松比匹配。芯材主要通过塑性压缩损伤和剪切断裂破坏吸收能量,而表层吸能则主要通过环向的花瓣形拉伸断裂破坏。研究表明,该型结构单元压缩吸能特性优异,可实现海洋工程结构平台的防护吸能和浮力储备要求。     

卫星中心承力筒结构优化设计研究

利用有限元软件ANSYS建立复合材料中心承力筒式卫星平台结构的参数化有限元分析模型,计算了整星结构振动模态,在此基础上对复合材料蜂窝夹层中心承力筒结构分析模型进行简化,在满足结构的强度、变形、振动和屈曲约束条件下,对承力筒结构进行优化设计,并对多种方案进行比较,提出的方法和思路为今后同类结构设计提供了参考。     

复合材料层合结构层向理论及应用进展

层向理论是由Reddy提出来的一种用于精确分析复合材料层合结构的三维板壳分析理论.由于不引入任何的变形和应力假设条件,因此相较于传统的等效单层板理论,层向理论在分析大厚度复合材料层合板壳结构的静动态响应及其局部层间效应时具有较大的优势.系统地综述了层向理论近年来的研究进展、数值解法及其应用情况.具体包括:层向理论的基本...     

宽带单脉冲雷达实测数据三维成像的平面视觉形态表示

针对宽带单脉冲雷达实测数据三维成像结果难以直观表示的问题,研究了平面视觉形态表示方法。所谓平面视觉形态,是指用设想的人眼沿着雷达波束方向观测得到的目标结构向适当平面的投影。为获得波束依赖平面视觉形态表示,给出了从实测数据中计算雷达波束方向的方法并从目标尺寸准确估计的角度分析了获取雷达波束方向的必要性,在确定波束方向的基础上,根据投影平面确定新的坐标系,并给出了从雷达观测坐标系到新坐标系的坐标旋转方法。给出了某民航飞机实测数据三维成像处理结果在雷达观测坐标系中的投影表示和新坐标系中的平面视觉形态表示,通过两种表示的对比分析,显示了平面视觉形态表示对特征提取的价值。     

灭火救援视景仿真中三维虚拟消防队员的设计与实现

灾害场景视景仿真是灭火救援计算机模拟训练系统的重要组成部分。而对于灾害场景中人的行为描述,特别是消防指战员组织实施灭火救援行动的描述是灾害场景表现的重要方面。从开发工具、角色建模、格式转化和骨骼动画等方面入手,就如何在灭火救援视景仿真中创建虚拟消防队员展开研究。结论表明：通过3dsMAX进行角色建模,通过Cal3D实现骨骼驱动的办法是实现三维虚拟消防队员的一个可行方案。     

多分辨率建模航空武器装备体系对抗效能评估

根据多分辨率建模的思想,分析航空武器装备体系对抗的特点,提出基于多分辨率建模的航空武器装备体系对抗效能评估模型框架,通过体系对抗过程物理特性的分析提炼数学描述方法,基于主动元建模技术建立从高分辨率实体仿真模型的仿真元模型,探讨了对仿真元模型进行基于马尔科夫链的串联聚合和基于元胞自动机的空间聚合方法,提出效能评估多维矢量空间指标体系,研究结果对我军航空武器装备效能评估以及作战论证都具有一定的指导意义和参考价值.     

双机空战模拟结果评判研究

定义了空战模拟结果指标-空战结果矢量和取胜矢量,推导了基于武器杀伤概率的取胜矢量计算方法,为定量研究作战飞机空战效能提供了依据。     

关于超百米建筑消防改造设计的分析与探讨

世纪大厦原设计建筑高度为99.8m,在施工过程中加层,导致该建筑超过100m,原消防设计已不能符合国家标准规范的相关规定,针对这一问题,对该建筑消防设计进行分析和探讨,提出了合理的消防设计修改方案,为此类建筑的消防设计审核提供参考。     

Three-dimensional coordinates test method with uncertain projectile proximity explosion position based on dynamic seven photoelectric detection screen

To objectively obtain the three-dimensional coordinates of the projectile fuze proximity explosion when projectile intersects the head of missile target, we propose a dynamic seven photoelectric detection screen test method, which is made up of six plane detection screens and a flash photoelectric dynamic detection screen. The three-dimensional coordinates calculation model of the projectile proximity explosion position based on seven plane detection screens with dynamic characteristics is established. According to the relation of the dynamic seven photoelectric detection screen planes and the time values, the analytical function of the projectile proximity explosion position parameters under non-linear motion is derived. The projectile signal filtering method based on discrete wavelet transform is explored in this work. Additionally, the projectile signal recognition algorithm using an improved particle swarm is proposed. Based on the characteristics of the time duration and the signal peak error for the projectile passing through the detection screen, the signals attribution of the same projectile passing through six detection screens are analyzed for obtaining precise time values of the same projectile passing through the detection screens. On the basis of the projectile fuze proximity explosion test, the linear motion model and the proposed non-linear motion model are used to calculate and compare the same group of projectiles proximity explosion position parameters. The comparison of test results verifies that the proposed test method and calculation model in this work accurately obtain the actual projectile proximity explosion position parameters.     

Damage to aircraft composite structures caused by directed energy system: A literature review

This paper presents a comprehensive review of the research studies on direct energy system effect on aircraft composite structures to develop a good understanding of state-of-the-art research and devel-opment in this area. The review begins with the application of composite materials in the aircraft structures and highlights their particular areas of application and limitations. An overview of directed energy system is given. Some of the commonly used systems in this category are discussed and the working principles of laser energy systems are described. The experimental and numerical studies re-ported regarding the aircraft composite structures subject to the effect of directed energy systems, especially the laser systems are reviewed in detail. In particularly, the general effects of laser systems and the relevant damage mechanisms against the composite structures are reported. The review draws attention to the recent research and findings in this field and is expected to guide engineers/researchers in future theoretical, numerical, and experimental studies.